Boeing 767-323
Service difficulty reports · 8,544
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '767323' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '767323' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR NACA2022050500001None · noneDURING ENGINE #2 BORESCOPE INSPECTION FOUND FUEL PUMP LEAKING. (FUEL IN AND FUEL OUT PORTS) REMOVED AND REPLACED FUEL/OIL HEAT EXCHANGER GASKETS IAW B767 AMM 79-21-01, PERFORMED ENGINE GROUND TEST - IDLE POWER OPS AND LEAK CHECK GOOD PER AMM 71-00-00SDR NACA2022050300001None · noneREF TO REA 47303REA24 INTERIM REPAIR SEAT TRACK MAIN CARGO DECK STA 785 RBL 88.5. DEFERRED THE DAMAGED SEAT TRACK PER 49303REA24 AND NAC GMM DMI 5:31 SECTION 2 FOR MAINT TRACKING. PERMANENTLY REPAIR OR REPLACE THE DAMAGE SEAT TRACK LOC AT STA 785, RBL 88.5 BEFSDR NACA2022042900002None · noneLEFT ENGINE #2 IGNITION IS INTERMITTENT. DEFERRED LEFT ENGINE #1 IGNITION IAW MEL 74-00-01A CAT A 042922 0849Z. REMOVED AND REPLACED LEFT ENGINE #2 IGNITOR IAW B767 AMM 74-21-02. AUDIBLE TEST GOOD PER TASK 74-00-00-705-025-H00SDR NACA2022042900001None · noneLEFT PACK TEMP EICAS MESSAGE, PERFORMED QRH PROCEDURE, DID NOT CLEAR. PERFORMED OPS CHECK OF LH PACK TEMP CONTROL IAW 21-51-00. NO FAULTS NOTED AND MESSAGE CLEARED. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR MK1Y20220429011None · noneEXTERNAL FUSELAGE SKINS, STA 390, STR-24R; STA 396, STR-22R; STA 1420, STR-31L – STR-32L; STA 1351, STR-31R: DURING MAINTENANCE INSPECTION AT IAI, A FEW BLENED OUTS WERE FOUND ON FUSELAGE SKINS 141T3330, 146T3230, 146T3530 AT LOCATIONS AS MENTIONED ABOVE. SEE SDR MK1Y20220429010None · noneDURING MAINTENANCE INSPECTION, LIGHTNING STRIKE DAMAGE WAS FOUND ON EXTERNAL FUSELAGE SKIN AT DATUM LOCATION. THE DAMAGE WAS REMOVED BY BLENDING IN THE FASTENERS AREA.SDR MK1Y20220429009None · noneTAILCONE ASSY, STA 1943.50 TO STA 1952.00: DURING MAINTENANCE INSPECTION MULTIPLE LIGHTING STRIKES WERE FOUND ON TAILCONE ASSY 148T8301-1 (148T8301-1 7 -2 SKINS). THE DAMAGES WERE BLENDED OUT AS REQUIRED, AND NDT HAS PERFORMED REMAINING MATERIAL THICKNESS AND SDR MK1Y20220429008None · noneL/H WING, OUTBD TRAILING EDGE FLAP (P/N: 113T3100-95G, S/N: 000251): DURING MAINTENANCE INSPECTION AT IAI, AN UNDOCUMENTED REPAIR WITH LIGHT CORROSION WAS FOUND ON THE LOWER SKIN PANEL OF THE FLAP AT APPROXIMATELY OTEF 300.88. AFTER THE REPAIR WAS DIMANTLED, ASDR MK1Y20220429007None · noneFUSELAGE FRAME, STA 1461, STR-4R – STR-5R: DURING MAINTENANCE INSPECTION AT IAI, CRACKS WERE FOUND AT DATUM LOCATION. SEE RFTA 02815-0223. THE DAMAGE WAS REMOVED PER J/C MF02815R0223-01 INSTRUCTIONS. THE CUTOUT IS ABOVE 1.99X0.73 INCH.SDR MK1Y20220429006None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, RBL 28.33, STR-U10: DURING MAINTENANCE INSPECTION, CORROSION DAMAGE WAS FOUND AT DATUM LOCATION AS MENTIONED ABOVE. THE CORROSION WAS REMOVED AND REMAINING MATERIAL THICKNESS MEASUREMENT WAS PERFORMED.SEE RFTASDR MK1Y20220429005None · noneENGINE # 1 LH CORE COWL HAT FRAME NAC STA 303.75, MID LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, A 1.2 INCH CRACK WAS FOUND ON THE ENG # 1 L/H CORE COWL AFT HAT FRAME P/N 224-2318. THE AFT HAT FRAME FALLS UNDER ZONE CC2 AS PER TABLE 101 B767-300 SRMSDR MK1Y20220429004None · noneEXTERNAL FUSELAGE SKIN, SECTION 41, STA 168, BELOW STR-21R; 141T3211: DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLENSDR MK1Y20220429003None · noneSTA 132.5 – STA 172.5, ABOVE STR-21L:
DURING MAINTENANCE INSPECTION AT IAI, MULTIPLE EXISTING UNDOCUMENTED BLEND OUTS WERE FOUND ON THE EXTERNAL FUSELAGE SKIN. ALSO, A GOUGE WAS FOUND ON THE EDGE OF THE DATUM SKIN, STA 132.5.SDR MK1Y20220429002None · noneEXTERNAL FUSELAGE SKIN, SECTION 46, STA 1485, STR-37R; 146T3240:
DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND ON THE EXTERNAL FUSELAGE SKINS AT STA 1485, STR-37R. THE AFFECTED FASTENER IN THE BLEND OUT AREA WAS REMOVED. AFTER INSPECTISDR MK1Y20220429001None · noneEXTERNAL FUSELAGE SKIN - STA 1261.5, STR 28R-STR 29R:DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND , COMMON TO THE FASTENER, THAT IS NOT ALLOWED PER B767-300 SRM 53-00-01, AD1.SDR NACA2022042500001Controller · failedAT CRUISE LEFT ENGINE HPSOV EICAS ILLUMINATED, PERFORMED QRH. PER FIM 36-10 FAULT TREE 853 WAS REPLACED LEFT ENGINE HPC IAW AMM 36-11-08/401, INSTALLATION TEST NORMAL. NO TRAX INFO FOR UNIT.SDR NACA2022042400001None · noneLEFT FORWARD FUEL PMP SWITCH LIGHTS INOP IN FLIGHT ONLY. OPS CHECKED LEFT FWD FUEL PUMP SWITCH LIGHT PER AMM 28-22-00, OPS CHECK OKAY ON THE GROUND.SDR NACA2022042300001None · noneLEFT PACK TEMP MSG ON EICAS ON GROUND - DURING PREFLIGHT. PERFORMED BITE TEST L PACK SYSTEM IS OK FOR NOW REF 21-60-00 NO DEFECTS NOTED.SDR NACA2022042200003None · nonePOST FLIGHT WALK-AROUND FOUND LH WING OB FLAP INBOARD SIDE DELAMINATED APPROX 18X18". CORRECTIVE ACTION IN WORK.SDR NACA2022042200005None · noneRIGHT ENGINE IDG DPI EXTENDED. REMOVED AND REPLACED RIGHT IDG FILTER IAW B767 AMM 24-11-02 OPS CHECK NORMAL, NO LEAKS NOTED.SDR NACA2022042200004None · noneECS/MSG DC FUEL PUMP ON MTX MSG. CLEANED CONNECTOR D156C @ S74 REF SWPM 20-26-01. PERFORMED OPS APU FUEL FEED SYST OPS CHECK OK IAW AMM 28-25-00SDR NACA2022042200002None · missingFOUND APU LEFT AFT VIBRATION ISOLATOR MISSING RETAINING NUT AND APU NOT FULLY SECURED. DEFERRED APU INOP PER MEL 49-11-01A CAT C ON 4/23/2022. REMOVED AND REPLACED LEFT AFT VIBRATION ISOLATOR IAW AMM 49-13-02. ACFT RELEASED NO ETOPS. NO TIME INFO ON TRAX.SDR NACA2022042200001Modulating Valve · failedAFT CABIN TEMP EICAS MSG. AFT CABIN TEMP EICAS MSG DEFERRED PER MEL 21-61-01-02 CAT C @ 0927Z, 4/22/22 AC REMAINS ETOPS 180. CLEARED MEL 21-61-02-02 REMOVED AND REPLACED AFT ZONE TRIM MODULATING VALVE PER AMM 21-61-07 @0530Z 4/23/22 AC REMAINS ETOPS 180. NO TRSDR NACA2022041900001None · noneAPU OIL COOLING FLEXIBLE DUCTS WORN/TORN, FORWARD AND AFT. REPLACED BOTH FWD AND AFT FLEXIBLE DUCTS PER AMM 49-51-01SDR NACA2022041800001Switch · failedAPU FAILED TO START. DEFERRED PER MEL 49-11-01A CAT C ON 4/19/22. REMOVED AND REPLACED DEICE VALVE SOLENOID AS PER REF B767 AMM 49-27-08 PERFORMED OPS CHECK NORMAL NO LEAKS. REQUIRED COLD SOAK START FOR ETOPS 180. NO TRAX TIME INFO AVAILABLE.SDR NACA2022041700001Fan · failedSTATUS MSG "FWD EQ EXH FAN" ON THE GROUND IN MDSD. DEFERRED PER MEL 21-58-04 ON 4-17-22 AT 1515 CAT C. PLACARD INSTALLED ACCOMPLISHED MX PROCEDURES. REMOVED AND REPLACED FWD EQUIP EXH FAN AS PER REF B767 AMM 21-58-06 PERFORMED OPS CHECK, FOUND NORMAL.SDR NACA2022041600002Switch · failedTROUBLESHOOT FAULT MESSAGES ON APU HEALTH CHECK GEN FILTER. WHILE RUNNING APU, AUTO SHUTDOWN WITH GEN FILTER MSG. PERFORMED FIM 49-11 FT 969. REPLACED GENERATOR OIL FILTER AP SWITCH WITH OPS CHECK GOOD PER AMM 49-27-15. GROUND VERIFIED AND AC REMAINS ETOPS 180SDR NACA2022041600001None · noneL HF RADIO INOP. PLACED ON MEL IAW MEL 23-11-01-02A CAT D 16 APR 1538Z, AIRCRAFT IS NOT ETOPS 180, PLACARD TURNED TO NON-ETOPS 180. REMOVED AND REPLACE L HF COMM IAW AMM 23-11-01-12, OPS CHECK GOOD NO DEFECTS NOTED. NO TIMES AVAILABLE IN TRAX.SDR NACA2022041300002None · noneSUPPLEMENTAL INFORMATION. CORRECTING CONTROL NUMBER VS NACA2022041300001SDR NACA2022041300001None · noneAPU FAULT WOULD NOT START ON GROUND IN MIA. ACCOMPLISHED APU BITE PER FIG 49-11 FAULT TREE TO958, SELF-TEST OK, APU STARTS NORMALLYSDR NACA2022040900001None · noneLEFT ENGINE PRV STATUS ILLUMINATED. PERFORMED FIM 36-10 FAULT TREE 847. FOUND ONE OF PRV TERMINAL LUG NUT LOOSE. RE-TIGHTENED PRV TERMINAL NUT PER AMM 36-11-18. PERFORMED IDLE RUN ON LEFT ENGINE PER AMM 71-00-00. OPS CHECK GOOD. NO MESSAGES ETOPS VERIFICATION SDR IXXA2022040602Duct · chafed#1 PYLON ANTI ICE DUCT CHAFEDSDR NACA2022040300001Controller · failedSUPPLEMENTAL INFORMATION - REMOVED AND REPLACED APU CONTROLLER IAW B767 AMM 49-61-05 OPS CHECK NORMAL NO TIME INFO ON TRAX.SDR IXXA2022040101Rub Strip · crackedREPAIR - CHAFE STRIP BEHIND ENGINE MOUNT ACCESS PANEL 436AL BROKEN OFF NAC 203-NAC 203SDR NACA202203290001None · noneAPU WOULD NOT START AFTER LANDING IN MIA. NO ENGINE ROTATION ON APU. PERFORMED APU ECU BITE PER B767 AMM 49-61-05 NO DEFECT NOTED. PERFORMED OPS CHECK OF APU PER B767 AMM 49-11-00, APU CHECKS GOOD. ETOPS GROUND VERIFICATION COMPLETED.SDR NACA2022032800002Valve · failedAFT CABIN TEMP EICAS MSG AND DISCRETE LIGHT ON. REMOVED AND REPLACED AFT TRIM AIR MODULATING VALVE, OPS CHECK AS PER AMM 21-61-07 AC REMAINS ETOPS 180. NO TIME INFO IN TRAX.SDR NACA2022032800001None · noneLEFT EEC INOP ON TAXI. DEFERRED LEFT EEC IAW MEL 73-21-01-01B CAT C. PERFORMED TS IAW FIM 71-01 FAULT TREE 823, ALSO PERFORMED LEFT ENGINE PMC CONNECTOR CLEANING IAW SWPM 20-60-01, PMC END TEST NORMAL IAW AMM 73-21-07/501. AC RELEASED ETOPS 180SDR IXXA2022040403None · crackedO/B UPPER ATTACH FITTING AFT OF PNL 446AR IS CRACKEDSDR NACA2022032700001None · noneCHECK APU OIL, CHECK FOR LEAK. DEFERRED PER MEL 49-11-01A CAT C ON 3/27/22 AT 1920Z AIRCRAFT REMAINS NON-ETOPS. ADJUSTED OIL CAPS LOCKING MECHANISM ACCOMPLISHED LEAK CHECK APU OPS CHECK, NO LEAKS NOTED DURING TWO HOURS CHECK.SDR IXXA2022040402Frame · cracked#2 PYLON INTERNAL FRAME IS CRACKED @ UPPER I/B FASTENER HOLE ON O/B SIDE OF PYLON AFT OF PNL 446ARSDR IXXA2022040110Bushing · corroded#1 PYLON O/B SIDE LINK UPPER FWD BUSHING IS PITTEDSDR IXXA2022040109None · corroded#1 PYLON UPPER LINK UPPER BUSHING IS PITTEDSDR IXXA2022040108None · corroded#2 PYLON UPPER LINK UPPER BUSHING IS PITTEDSDR NACA2022032500001None · noneSUPPLEMENTAL INFORMATION: REMOVED AND REPLACED #2 IGNITOR PLUG IAW AMM 74-21-01 ACCOMPLISHED OPS CHECK FOUND GOOD. AC REMAINS NO ETOPS.SDR IXXA2022040107Fitting · wornNO.2 PYLON O/B T/R OPENING ACTUATOR, UPPER PYLON BRACKET DAMAGED AT ATTACH BUSHINGSDR IXXA2022040106Stiffener · crackedBRACKET JUST UNDER FWD END OF HYD BAY DOOR SILL BEAM FOUND CRACKEDSDR IXXA202203257015Autopilot Sys · faultedENROUTE FROM KONT TO KPHI AND APPROACHING 8,000 AUTOPILOT WOULD NOT DISENGAGE. AIR TURN BACK TO KONT WITH EMERGENCY DESCENT. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. UPON ARRIVAL AIRCRAFT WAS GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK SDR IXXA2022040111None · crackedI/B UPPER ATTACH FITTING AFT OF PNL446AL CRACKEDSDR IXXA2022040103Frame · crackedO/B FRAME JUST AFT OF PNL 436AL DAMAGED, NAC 285.45 TO NAC 285.45SDR IXXA2022040102Stiffener · crackedO/B T-FITTING TOP FLANGE MISSING/DAMAGED JUST AFT OF PNL 436AL NAC 278 - NAC 288
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